CA2594008C - Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge - Google Patents
Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge Download PDFInfo
- Publication number
- CA2594008C CA2594008C CA2594008A CA2594008A CA2594008C CA 2594008 C CA2594008 C CA 2594008C CA 2594008 A CA2594008 A CA 2594008A CA 2594008 A CA2594008 A CA 2594008A CA 2594008 C CA2594008 C CA 2594008C
- Authority
- CA
- Canada
- Prior art keywords
- downstream
- annular
- air
- diffuser
- impeller
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0606541 | 2006-07-19 | ||
| FR0606541A FR2904036B1 (fr) | 2006-07-19 | 2006-07-19 | Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2594008A1 CA2594008A1 (fr) | 2008-01-19 |
| CA2594008C true CA2594008C (fr) | 2014-11-04 |
Family
ID=37770941
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2594008A Active CA2594008C (fr) | 2006-07-19 | 2007-07-16 | Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US7942630B2 (https=) |
| EP (1) | EP1882826B1 (https=) |
| JP (1) | JP4956809B2 (https=) |
| CA (1) | CA2594008C (https=) |
| FR (1) | FR2904036B1 (https=) |
| RU (1) | RU2433310C2 (https=) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8075247B2 (en) * | 2007-12-21 | 2011-12-13 | Pratt & Whitney Canada Corp. | Centrifugal impeller with internal heating |
| US8147178B2 (en) * | 2008-12-23 | 2012-04-03 | General Electric Company | Centrifugal compressor forward thrust and turbine cooling apparatus |
| US8087249B2 (en) * | 2008-12-23 | 2012-01-03 | General Electric Company | Turbine cooling air from a centrifugal compressor |
| US9228497B2 (en) | 2010-12-30 | 2016-01-05 | Rolls-Royce Corporation | Gas turbine engine with secondary air flow circuit |
| GB2510004B (en) * | 2013-08-19 | 2015-10-14 | Rolls Royce Plc | Axial flow machine cooling system |
| FR3025260B1 (fr) * | 2014-08-29 | 2019-08-30 | Safran Aircraft Engines | Compresseur centrifuge a resistance amelioree |
| US10208668B2 (en) * | 2015-09-30 | 2019-02-19 | Rolls-Royce Corporation | Turbine engine advanced cooling system |
| US10830144B2 (en) | 2016-09-08 | 2020-11-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine compressor impeller cooling air sinks |
| JP6750998B2 (ja) * | 2016-10-07 | 2020-09-02 | パナソニックi−PROセンシングソリューションズ株式会社 | 監視システム及び監視方法 |
| FR3062682B1 (fr) * | 2017-02-07 | 2019-04-19 | Safran Aircraft Engines | Partie de turbomachine comprenant une paroi de separation de deux cavites pourvue de bossages |
| CN107725479B (zh) * | 2017-09-26 | 2019-09-24 | 中国科学院工程热物理研究所 | 一种旋转盘腔内部的转子罩壳结构及包含该结构的发动机 |
| US11049176B1 (en) | 2020-01-10 | 2021-06-29 | House Of Skye Ltd | Systems/methods for identifying products within audio-visual content and enabling seamless purchasing of such identified products by viewers/users of the audio-visual content |
| US11525393B2 (en) | 2020-03-19 | 2022-12-13 | Rolls-Royce Corporation | Turbine engine with centrifugal compressor having impeller backplate offtake |
| FR3137409A1 (fr) * | 2022-07-04 | 2024-01-05 | Safran Helicopter Engines | Compresseur pour aéronef |
| US11773773B1 (en) | 2022-07-26 | 2023-10-03 | Rolls-Royce North American Technologies Inc. | Gas turbine engine centrifugal compressor with impeller load and cooling control |
| FR3160436B1 (fr) * | 2024-03-19 | 2026-03-20 | Safran Aircraft Engines | système de contrôle de la pressurisation d’une cavité aval de rotor de compresseur centrifuge dans une turbomachine |
| FR3166163A1 (fr) | 2024-09-06 | 2026-03-13 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
| FR3166167A1 (fr) | 2024-09-06 | 2026-03-13 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
| FR3166178A1 (fr) | 2024-09-06 | 2026-03-13 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
| FR3166164A1 (fr) | 2024-09-06 | 2026-03-13 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
| FR3166165A1 (fr) | 2024-09-06 | 2026-03-13 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE968742C (de) * | 1944-09-22 | 1958-03-27 | Daimler Benz Ag | Mehrstufiges Radialgeblaese, vorzugsweise Ladegeblaese fuer Flugmotoren |
| GB1047014A (en) * | 1962-07-03 | 1966-11-02 | English Electric Co Ltd | Improvements in or relating to hydraulic pumps, turbines or reversible pump turbines |
| FR1472085A (fr) * | 1965-11-18 | 1967-03-10 | Snecma | Perfectionnement aux compresseurs contra-rotatifs |
| US3469772A (en) * | 1967-07-19 | 1969-09-30 | Donald A Mcdonald | Air moving apparatus |
| US4462204A (en) * | 1982-07-23 | 1984-07-31 | General Electric Company | Gas turbine engine cooling airflow modulator |
| SU1222900A1 (ru) * | 1984-11-22 | 1986-04-07 | Производственное объединение "Невский завод" им.В.И.Ленина | Сигнализатор помпажа турбокомпрессора |
| JPS62143098A (ja) * | 1985-12-18 | 1987-06-26 | 松下電器産業株式会社 | 明瞭度評価用単音節の合成方法 |
| DE4225625A1 (de) * | 1992-08-03 | 1994-02-10 | Asea Brown Boveri | Abgasturbolader |
| GB2290113B (en) * | 1994-05-31 | 1998-07-15 | Ingersoll Dresser Pump Co | Centrifugal pump |
| US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
| JPH1089291A (ja) * | 1996-09-11 | 1998-04-07 | Tochigi Fuji Ind Co Ltd | 遠心式コンプレッサ |
| US5996331A (en) * | 1997-09-15 | 1999-12-07 | Alliedsignal Inc. | Passive turbine coolant regulator responsive to engine load |
| US6035627A (en) * | 1998-04-21 | 2000-03-14 | Pratt & Whitney Canada Inc. | Turbine engine with cooled P3 air to impeller rear cavity |
| DE59809867D1 (de) * | 1998-05-25 | 2003-11-13 | Abb Turbo Systems Ag Baden | Radialverdichter |
| JP2001123997A (ja) * | 1999-10-21 | 2001-05-08 | Hitachi Ltd | 磁気軸受搭載遠心圧縮機 |
| JP4375883B2 (ja) * | 2000-06-02 | 2009-12-02 | 本田技研工業株式会社 | ガスタービンエンジンの軸受へのシールエア供給装置 |
| US6276896B1 (en) * | 2000-07-25 | 2001-08-21 | Joseph C. Burge | Apparatus and method for cooling Axi-Centrifugal impeller |
| RU2208177C1 (ru) * | 2002-07-15 | 2003-07-10 | Открытое акционерное общество Авиамоторный научно-технический комплекс "Союз" | Двухконтурный турбореактивный двигатель |
| JP4125985B2 (ja) * | 2003-03-31 | 2008-07-30 | 株式会社山田製作所 | ウォーターポンプ |
| DE10325980A1 (de) * | 2003-06-07 | 2004-12-23 | Daimlerchrysler Ag | Abgasturbolader |
-
2006
- 2006-07-19 FR FR0606541A patent/FR2904036B1/fr active Active
-
2007
- 2007-06-29 EP EP07290824A patent/EP1882826B1/fr active Active
- 2007-07-16 CA CA2594008A patent/CA2594008C/fr active Active
- 2007-07-17 US US11/779,016 patent/US7942630B2/en active Active
- 2007-07-18 RU RU2007127561/06A patent/RU2433310C2/ru active
- 2007-07-18 JP JP2007186669A patent/JP4956809B2/ja active Active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2007127561A (ru) | 2009-01-27 |
| US20100028137A1 (en) | 2010-02-04 |
| RU2433310C2 (ru) | 2011-11-10 |
| FR2904036A1 (fr) | 2008-01-25 |
| US7942630B2 (en) | 2011-05-17 |
| JP2008025578A (ja) | 2008-02-07 |
| JP4956809B2 (ja) | 2012-06-20 |
| EP1882826B1 (fr) | 2012-08-01 |
| CA2594008A1 (fr) | 2008-01-19 |
| FR2904036B1 (fr) | 2008-08-29 |
| EP1882826A1 (fr) | 2008-01-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MPN | Maintenance fee for patent paid |
Free format text: FEE DESCRIPTION TEXT: MF (PATENT, 18TH ANNIV.) - STANDARD Year of fee payment: 18 |
|
| U00 | Fee paid |
Free format text: ST27 STATUS EVENT CODE: A-4-4-U10-U00-U101 (AS PROVIDED BY THE NATIONAL OFFICE); EVENT TEXT: MAINTENANCE REQUEST RECEIVED Effective date: 20250707 |
|
| U11 | Full renewal or maintenance fee paid |
Free format text: ST27 STATUS EVENT CODE: A-4-4-U10-U11-U102 (AS PROVIDED BY THE NATIONAL OFFICE); EVENT TEXT: MAINTENANCE FEE PAYMENT PAID IN FULL Effective date: 20250707 |